The invention discloses a mechanical property experiment device and method for an aileron driving mechanism, the experiment device comprises a to-be-experimented driving mechanism and an experiment tool, the driving mechanism comprises a driving rod and a carbon tube, the diameter of the carbon tube is greater than that of the driving rod, and the carbon tube is sleeved outside the driving rod; the experiment tool comprises a loading mechanism, a torsion fixing mechanism, an angle measuring mechanism and a plurality of height adjusting mechanisms, the two ends of the driving rod extend out of openings in the two ends of the carbon tube respectively, one extending end is connected with the loading mechanism, torque to be tested is applied by the loading mechanism, and the end is further connected with the angle measuring mechanism; the other extending end is detachably connected with the torsion fixing mechanism, and the multiple height adjusting mechanisms are evenly distributed in the axial direction of the carbon tube and movably support the carbon tube in the vertical direction. The experimental device has the advantages of being simple in structure, good in simulation, capable of providing rich experimental situations and the like. The experimental method has the advantages of being simple in step, easy and convenient to operate, capable of obtaining mechanical property results with high accuracy and the like.
本发明公开了一种副翼驱动机构的力学性能实验装置及方法,实验装置包括待实验的驱动机构和实验工装,驱动机构包括驱动杆和碳管,碳管的直径大于驱动杆的直径,碳管套接在驱动杆的外部;实验工装包括加载机构、扭转固定机构、角度测定机构和多个高度调节机构,驱动杆的两端分别从碳管的两端开口处伸出,且一伸出端连接加载机构,由加载机构施加待实验扭矩,该端还连接有角度测定机构,另一伸出端可拆卸连接扭转固定机构,多个高度调节机构沿碳管的轴向均匀分布,并沿竖直方向活动托持碳管。本发明的实验装置具有结构简单、拟真性好和能够提供丰富的实验情形等优点,实验方法具有步骤简单、操作简便和能够获取精准度较高的力学性能结果等优点。
Mechanical property experiment device and method for aileron driving mechanism
一种副翼驱动机构的力学性能实验装置及方法
2022-04-26
Patent
Elektronische Ressource
Chinesisch
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Integral wing and aileron driving device and mounting method
Europäisches Patentamt | 2022
|